Multi-rotor vehicle with edge computing systems

ABSTRACT

A multi-rotor vehicle includes a plurality of electric motors and edge computing systems (ECSs). The electric motors are operatively coupled to respective rotors, and cause the respective rotors to rotate relative to the airframe. The ECSs are independent, distinct and distributed to the electric motors, each operatively coupled to a respective electric motor and thereby a respective rotor. Each ECS is configured to acquire and process sensor data for the respective rotor to determine rotor status information, and execute motor commands to control the respective electric motor and thereby the respective rotor. Each ECS is configured as an integrated flight computer and motor controller.

CROSS-REFERENCE TO RELATED APPLICATION(S)

The present application claims priority to U.S. Provisional PatentApplication No. 62/814,349, entitled: Multi-Rotor Vehicle with EdgeComputing Systems, filed on Mar. 6, 2019, the content of which isincorporated herein by reference in its entirety.

TECHNOLOGICAL FIELD

The present disclosure relates generally to vehicles and, in particular,to multi-rotor vehicles.

BACKGROUND

A multi-rotor vehicle is generally a vehicle with more than one rotor,typically more than two rotors. A primary example of a multi-rotorvehicle is a non-fixed wing aircraft, referred to as a rotorcraft orrotary-wing aircraft. This multi-rotor vehicle is an aircraft that useslift generated by wings or propellers, referred to as rotary wings,rotor blades or more simply rotors, that revolve around a mast. Arotorcraft may include one or multiple rotors mounted on a single mastor multiple masts. For example, a quadcopter is a multi-rotor rotorcraftthat generates lift via four rotors. Other examples include a tricopter,hexacopter and octocopter that include respectively three, six and eightrotors. A rotorcraft may be an unmanned rotorcraft controlled via aremote communications station and/or programmed instructions, althoughin other examples, a rotorcraft may be a manned vehicle.

Multi-rotor rotorcraft typically include a centrally-located flightcontroller, which makes it a single point of failure. Most flightcontrol computers and sensors are triple redundant to improve flightworthiness; however, this requires control forces (control rods),actuator communication and sensor communication must be routed from thecentral flight controller to each actuator on the rotorcraft. Thisequates to added weight and complexity.

Therefore it would be desirable to have a system and method that takesinto account at least some of the issues discussed above, as well asother possible issues.

BRIEF SUMMARY

Example implementations of the present disclosure are directed to amulti-rotor vehicle with distributed modular-based edge computingsystems that may be embedded with an integrated flight and motor controlsystem for each rotor. The edge computing systems may also include oneor more communication interfaces for communication with others of theedge computing systems, and/or remote stations. The modular-based edgecomputing systems of example implementations may increase thereliability and survivability of the multi-rotor vehicle.

The present disclosure thus includes, without limitation, the followingexample implementations.

Some example implementations provide a multi-rotor vehicle comprising:an airframe; and coupled to the airframe, a plurality of electric motorsoperatively coupled to a respective plurality of rotors, the pluralityof electric motors configured to cause the respective plurality ofrotors to rotate relative to the airframe; and a plurality of edgecomputing systems that are independent, distinct and distributed to theplurality of electric motors, each edge computing system of theplurality of edge computing systems operatively coupled to a respectiveelectric motor of the plurality of electric motors, and thereby arespective rotor of the respective plurality of rotors, each edgecomputing system configured to acquire and process sensor data for therespective rotor to determine rotor status information, and executemotor commands to control the respective electric motor and thereby therespective rotor, wherein each edge computing system is configured as anintegrated flight computer and motor controller.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, each edge computing system includes first powerdistribution circuitry for the flight computer, and second powerdistribution circuitry for the motor controller.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, each edge computing system further includes apower inverter circuit coupled to the second power distributioncircuitry, the power inverter circuit configured to supply power to therespective electric motor of the edge computing system.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, each edge computing system includes: processingcircuitry configured to acquire and process the sensor data for therespective rotor to determine rotor status information, and execute themotor commands to control the respective electric motor and thereby therespective rotor; and a communication interface configured to enable theedge computing system to communicate with others of the plurality ofedge computing systems.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, the plurality of edge computing systems areconfigured according to a model in which any of the plurality of edgecomputing systems is selectable as a primary edge computing system, andthe plurality of edge computing systems other than the primary edgecomputing system are operable as secondary edge computing systems, thesecondary edge computing systems configured to communicate respectiverotor status information to the primary edge computing system, and theprimary edge computing system configured to provide the motor commandsto the secondary edge computing systems.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, each edge computing system further includes asecond communication interface configured to enable the edge computingsystem to communicate with a remote station, the primary edge computingsystem among the plurality of edge computing systems being configured tocommunicate with the remote station.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, the processing circuitry of each edge computingsystem further includes a clock to measure and keep time at the edgecomputing system, the secondary edge computing systems configured tocommunicate with the primary edge computing system via respectivecommunication interfaces to synchronize respective clocks of thesecondary edge computing systems with the clock of the primary edgecomputing system.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, the primary edge computing system is configuredto implement the flight computer to determine attitude, position andheading of the multi-rotor vehicle, and provide the motor commands basedon the rotor status information for the respective plurality of rotors,and the attitude, position and heading.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, each edge computing system includes an inertialmeasurement unit (IMU) and magnetometer, and the IMU and magnetometer ofthe primary edge computing system are configured to determine theattitude, position and heading of the multi-rotor vehicle.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, each edge computing system is configured tostore a configuration file with an ordered list of the plurality of edgecomputing systems that begins with the primary edge computing system andthen a first of the secondary edge computing systems, and wherein theprimary edge computing system is configured to communicate health statusinformation to the first of the secondary edge computing systems, and inresponse, the first of the secondary edge computing systems isconfigured to determine a health status of the primary edge computingsystem from the health status information, and assume responsibility asthe primary edge computing system when the health status reaches apredetermined threshold.

In some example implementations of the multi-rotor vehicle of anypreceding example implementation, or any combination of any precedingexample implementations, the ordered list includes a second of thesecondary edge computing systems after the first of the secondary edgecomputing systems, and wherein after the first of the secondary edgecomputing systems assumes responsibility as the primary edge computingsystem, the second of the secondary edge computing systems assumesresponsibility as the first of the secondary edge computing systems.

Some example implementations provide an edge computing system of aplurality of edge computing systems configured for use on a multi-rotorvehicle including a plurality of electric motors operatively coupled toa respective plurality of rotors, the plurality of electric motorsconfigured to cause the respective plurality of rotors to rotaterelative to an airframe, the plurality of edge computing systems beingindependent, distinct and distributable to the plurality of electricmotors, the edge computing system comprising: processing circuitryoperatively coupleable to a respective electric motor of the pluralityof electric motors, and thereby a respective rotor of the respectiveplurality of rotors, the processing circuitry configured to acquire andprocess sensor data for the respective rotor to determine rotor statusinformation, and execute motor commands to control the respectiveelectric motor and thereby the respective rotor; and a communicationinterface configured to enable the edge computing system to communicatewith others of the plurality of edge computing systems, wherein the edgecomputing system is configured as an integrated flight computer andmotor controller.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the edge computing system further comprisesfirst power distribution circuitry for the flight computer, and secondpower distribution circuitry for the motor controller.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the edge computing system further comprises apower inverter circuit coupled to the second power distributioncircuitry, the power inverter circuit configured to supply power to therespective electric motor of the edge computing system.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the edge computing system is configured tocommunicate with the others of the plurality of edge computing systemsaccording to a model in which any of the plurality of edge computingsystems is selectable as a primary edge computing system, and theplurality of edge computing systems other than the primary edgecomputing system are operable as secondary edge computing systems, thesecondary edge computing systems configured to communicate respectiverotor status information to the primary edge computing system, and theprimary edge computing system configured to provide the motor commandsto the secondary edge computing systems.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the edge computing system further comprises asecond communication interface configured to enable the edge computingsystem to communicate with a remote station, the primary edge computingsystem among the plurality of edge computing systems being configured tocommunicate with the remote station.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the processing circuitry of the edge computingsystem further includes a clock to measure and keep time at the edgecomputing system, the secondary edge computing systems configured tocommunicate with the primary edge computing system via respectivecommunication interfaces to synchronize respective clocks of thesecondary edge computing systems with the clock of the primary edgecomputing system.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the primary edge computing system is configuredto implement the flight computer to determine attitude, position andheading of the multi-rotor vehicle, and provide the motor commands basedon the rotor status information for the respective plurality of rotors,and the attitude, position and heading.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the edge computing system further comprises aninertial measurement unit (IMU) and magnetometer, and the IMU andmagnetometer of the primary edge computing system are configured todetermine the attitude, position and heading of the multi-rotor vehicle.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the edge computing system is configured tostore a configuration file with an ordered list of the plurality of edgecomputing systems that begins with the primary edge computing system andthen a first of the secondary edge computing systems, and wherein theprimary edge computing system is configured to communicate health statusinformation to the first of the secondary edge computing systems, and inresponse, the first of the secondary edge computing systems isconfigured to determine a health status of the primary edge computingsystem from the health status information, and assume responsibility asthe primary edge computing system when the health status reaches apredetermined threshold.

In some example implementations of the edge computing system of anypreceding example implementation, or any combination of any precedingexample implementations, the ordered list includes a second of thesecondary edge computing systems after the first of the secondary edgecomputing systems, and wherein after the first of the secondary edgecomputing systems assumes responsibility as the primary edge computingsystem, the second of the secondary edge computing systems assumesresponsibility as the first of the secondary edge computing systems.

Some example implementations provide a method of operating a multi-rotorvehicle including a plurality of electric motors operatively coupled toa respective plurality of rotors, and a plurality of edge computingsystems that are independent, distinct and distributed to the pluralityof electric motors, each edge computing system of the plurality of edgecomputing systems operatively coupled to a respective electric motor ofthe plurality of electric motors, and thereby a respective rotor of therespective plurality of rotors, the method comprising each edgecomputing system: acquiring and processing sensor data for therespective rotor to determine rotor status information; and executingmotor commands to control the respective electric motor and thereby therespective rotor, wherein each edge computing system is configured as anintegrated flight computer and motor controller.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, each edge computing system includes first powerdistribution circuitry for the flight computer, second powerdistribution circuitry for the motor controller, and a power invertercircuit coupled to the second power distribution circuitry, and themethod further comprises the power inverter circuit supplying power tothe respective electric motor of the edge computing system.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, the plurality of edge computing systems are configuredaccording to a model in which any of the plurality of edge computingsystems is selectable as a primary edge computing system, and theplurality of edge computing systems other than the primary edgecomputing system are operable as secondary edge computing systems, themethod further comprising the secondary edge computing systemscommunicating respective rotor status information to the primary edgecomputing system, and the primary edge computing system providing themotor commands to the secondary edge computing systems.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, each edge computing system is enabled to communicatewith a remote station, and the method further comprises the primary edgecomputing system among the plurality of edge computing systemscommunicating with the remote station.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, each edge computing system includes a clock to measureand keep time at the edge computing system, and the method furthercomprises the secondary edge computing systems communicating with theprimary edge computing system to synchronize respective clocks of thesecondary edge computing systems with the clock of the primary edgecomputing system.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, the method further comprises the primary edge computingsystem implementing the flight computer to determine attitude, positionand heading of the multi-rotor vehicle, and providing the motor commandsbased on the rotor status information for the respective plurality ofrotors, and the attitude, position and heading.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, each edge computing system includes an inertialmeasurement unit (IMU) and magnetometer, and the method furthercomprises the IMU and magnetometer of the primary edge computing systemdetermining the attitude, position and heading of the multi-rotorvehicle.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, each edge computing system is configured to store aconfiguration file with an ordered list of the plurality of edgecomputing systems that begins with the primary edge computing system andthen a first of the secondary edge computing systems, and wherein themethod further comprises the primary edge computing system communicatinghealth status information to the first of the secondary edge computingsystems, and in response, the first of the secondary edge computingsystems determining a health status of the primary edge computing systemfrom the health status information, and assuming responsibility as theprimary edge computing system when the health status reaches apredetermined threshold.

In some example implementations of the method of any preceding exampleimplementation, or any combination of any preceding exampleimplementations, the ordered list includes a second of the secondaryedge computing systems after the first of the secondary edge computingsystems, and wherein the method further comprises, after the first ofthe secondary edge computing systems assumes responsibility as theprimary edge computing system, the second of the secondary edgecomputing systems assuming responsibility as the first of the secondaryedge computing systems.

These and other features, aspects, and advantages of the presentdisclosure will be apparent from a reading of the following detaileddescription together with the accompanying figures, which are brieflydescribed below. The present disclosure includes any combination of two,three, four or more features or elements set forth in this disclosure,regardless of whether such features or elements are expressly combinedor otherwise recited in a specific example implementation describedherein. This disclosure is intended to be read holistically such thatany separable features or elements of the disclosure, in any of itsaspects and example implementations, should be viewed as combinableunless the context of the disclosure clearly dictates otherwise.

It will therefore be appreciated that this Brief Summary is providedmerely for purposes of summarizing some example implementations so as toprovide a basic understanding of some aspects of the disclosure.Accordingly, it will be appreciated that the above described exampleimplementations are merely examples and should not be construed tonarrow the scope or spirit of the disclosure in any way. Other exampleimplementations, aspects and advantages will become apparent from thefollowing detailed description taken in conjunction with theaccompanying figures which illustrate, by way of example, the principlesof some described example implementations.

BRIEF DESCRIPTION OF THE FIGURE(S)

Having thus described example implementations of the disclosure ingeneral terms, reference will now be made to the accompanying figures,which are not necessarily drawn to scale, and wherein:

FIG. 1 illustrates a multi-rotor vehicle environment in accordance withexample implementations of the present disclosure;

FIG. 2 illustrates a multi-rotor vehicle according to some exampleimplementations;

FIG. 3 more particularly illustrates an edge computing system, accordingto example implementations;

FIG. 4 is a flowchart illustrating various steps in a method ofoperating a multi-rotor vehicle, according to example implementations;and

FIG. 5 illustrates an edge computing system including processingcircuitry and various components of the edge computing system coupledthereto, according to example implementations.

DETAILED DESCRIPTION

Some implementations of the present disclosure will now be describedmore fully hereinafter with reference to the accompanying figures, inwhich some, but not all implementations of the disclosure are shown.Indeed, various implementations of the disclosure may be embodied inmany different forms and should not be construed as limited to theimplementations set forth herein; rather, these example implementationsare provided so that this disclosure will be thorough and complete, andwill fully convey the scope of the disclosure to those skilled in theart. For example, unless otherwise indicated, reference something asbeing a first, second or the like should not be construed to imply aparticular order. Also, something may be described as being abovesomething else (unless otherwise indicated) may instead be below, andvice versa; and similarly, something described as being to the left ofsomething else may instead be to the right, and vice versa. Likereference numerals refer to like elements throughout.

FIG. 1 illustrates a multi-rotor vehicle environment 100 in accordancewith example implementations of the present disclosure. The multi-rotorvehicle environment is an example of an environment in which amulti-rotor vehicle 102 may operate. The multi-rotor vehicle isgenerally a vehicle such as a rotorcraft with more than one rotor,typically more than two rotors. These rotors are sometimes referred toas wings, propellers, rotary wings, rotor blades or the like, and eachrevolves around a mast coupled to a motor. As shown, the multi-rotorvehicle takes the form of a quadcopter, which may be manned or unmanned.Other examples of suitable multi-rotor vehicles include a manned orunmanned tricopter, hexacopter, octocopter or the like.

The multi-rotor vehicle 102 flies and may perform additional operationsin the multi-rotor vehicle environment 100. For example, the multi-rotorvehicle may perform operations for a surveillance mission. Theoperations for the surveillance mission may include generating images ofobjects including a building 104. These images may be still images,video, or some combination thereof. Additionally, the surveillancemission also may include generating images of traffic on road 106. Forexample, the multi-rotor vehicle may generate images of a vehicle 108moving on the road.

According to example implementations of the present disclosure, themulti-rotor vehicle 102 includes distributed modular-based edgecomputing systems that may increase the reliability and survivability ofthe multi-rotor vehicle. FIG. 2 illustrates a multi-rotor vehicle 200that may correspond to multi-rotor vehicle 102, according to someexample implementations of the present disclosure. As shown, themulti-rotor vehicle includes an airframe 202, and coupled to theairframe, a plurality of electric motors 204 operatively coupled to arespective plurality of rotors 206. The plurality of electric motors areconfigured to cause the respective plurality of rotors to rotaterelative to the airframe.

Also coupled to the airframe 202, the multi-rotor vehicle 200 includes aplurality of edge computing systems (ECS) 208 (shown operable asincluding primary and secondary edge computing systems 208 a, 208 b)that are independent, distinct and distributed to the plurality ofelectric motors (M) 204. Each edge computing system of the plurality ofedge computing systems is operatively coupled to a respective electricmotor of the plurality of electric motors, and thereby a respectiverotor of the respective plurality of rotors 206. Each edge computingsystem is configured to acquire and process sensor data for therespective rotor to determine rotor status information, and executemotor commands to control the respective electric motor and thereby therespective rotor. Examples of suitable sensor data include rotor statusinformation such as rotation direction, rotation speed, blade angle,altitude, wind and the like.

In some examples, the plurality of edge computing systems 208 areconfigured according to a model in which any of the plurality of edgecomputing systems is selectable as a primary edge computing system 208a, and the plurality of edge computing systems other than the primaryedge computing system are operable as secondary edge computing systems208 b. The secondary edge computing systems are configured tocommunicate respective rotor status information to the primary edgecomputing system, and the primary edge computing system is configured toprovide the motor commands to the secondary edge computing systems.

In some examples, each edge computing system 208 is configured to storea configuration file with an ordered list of the plurality of edgecomputing systems that begins with the primary edge computing system 208a and then a first of the secondary edge computing systems 208 b. Inthese examples, the primary edge computing system is configured tocommunicate health status information to the first of the secondary edgecomputing systems. In response, the first of the secondary edgecomputing systems is configured to determine a health status of theprimary edge computing system from the health status information, andassume responsibility as the primary edge computing system when thehealth status reaches a predetermined threshold.

In some further examples, the ordered list includes a second of thesecondary edge computing systems 208 b after the first of the secondaryedge computing systems. In these examples, after the first of thesecondary edge computing systems assumes responsibility as the primaryedge computing system 208 a, the second of the secondary edge computingsystems assumes responsibility as the first of the secondary edgecomputing systems.

FIG. 3 more particularly illustrates an edge computing system 208,according to example implementations of the present disclosure. Asshown, the edge computing system includes processing circuitry 310 and acommunication interface 312. The processing circuitry is configured toacquire and process the sensor data for the respective rotor of theplurality of rotors 206 to determine rotor status information, andexecute the motor commands to control the respective electric motor 204and thereby the respective rotor. And the communication interface isconfigured to enable the edge computing system to communicate withothers of the plurality of edge computing systems.

In some examples, the edge computing system 208 further includes asecond communication interface 314 configured to enable the edgecomputing system to communicate with a remote station 316. In theseexamples, the primary edge computing system 208 a among the plurality ofedge computing systems is configured to communicate with the remotestation. Examples of suitable remote stations include fixe or mobileground stations or terminals, other vehicles such as other aircraft,rotorcraft or the like.

In some examples, the processing circuitry 310 further includes a clock318 to measure and keep time at the edge computing system. In theseexamples, the secondary edge computing systems is configured tocommunicate with the primary edge computing system 208 a via respectivecommunication interfaces to synchronize respective clocks of thesecondary edge computing systems with the clock of the primary edgecomputing system.

In some examples, each edge computing system 208 is configured as anintegrated flight computer and motor controller. To this end, the edgecomputing system may include first power distribution circuitry 320 asuch as low-voltage power distribution circuitry for the flightcomputer, and second power distribution circuitry 320 b such ashigh-voltage power distribution circuitry for the motor controller. Insome further examples, the edge computing system includes a powerinverter circuit 322 coupled to the second power distribution circuitry,the power inverter circuit configured to supply power to the respectiveelectric motor 204 of the edge computing system.

In some examples, the primary edge computing system 208 a is configuredto implement the flight computer to determine attitude, position andheading of the multi-rotor vehicle 200, and provide the motor commandsbased on the rotor status information for the respective plurality ofrotors 206, and the attitude, position and heading. In some of theseexamples, each edge computing system 208 includes an inertialmeasurement unit (IMU) 324 and one or more navigation sensors 326 suchas a magnetometer. The IMU and magnetometer of the primary edgecomputing system are configured to determine the attitude, position andheading of the multi-rotor vehicle. In these examples, the IMU of theedge computing system is co-located with the respective rotor of theplurality of rotors 206. This may enable high bandwidth phasestabilization of local dynamic motor elastic modes without the need forhigh bandwidth sharing across multiple flight computers (no need toshare high frequency data with other flight computers).

FIG. 4 is a flowchart illustrating various steps in a method 400 ofoperating a multi-rotor vehicle 200, according to exampleimplementations of the present disclosure. As shown at 402 and 408, themethod includes each edge computing system 208 acquiring and processingsensor data for the respective rotor of the plurality of rotors 206 todetermine rotor status information, and executing motor commands tocontrol the respective electric motor 204 and thereby the respectiverotor. Again, the plurality of edge computing systems are configuredaccording to a model in which any of the plurality of edge computingsystems is selectable as a primary edge computing system 208 a, and theplurality of edge computing systems other than the primary edgecomputing system are operable as secondary edge computing systems 208 b.The method further includes the secondary edge computing systemscommunicating respective rotor status information to the primary edgecomputing system, and the primary edge computing system providing themotor commands to the secondary edge computing systems, as shown at 404and 406.

According to example implementations of the present disclosure, the edgecomputing system 208 and its components may be implemented by variousmeans. Means for implementing the edge computing system and itscomponents may include hardware, alone or under direction of one or morecomputer programs from a computer-readable storage medium. FIG. 5illustrates the edge computing system including its processing circuitry310 and various components of the edge computing system coupled to theprocessing circuitry for carrying out functions of the edge computingsystem such as those described herein. As shown, the edge computingsystem may include one or more of each of a number of components suchas, for example, the processing circuitry 310 connected to a memory 528(e.g., storage device).

The processing circuitry 310 may include one or more processors alone orin combination with one or more memories. The processing circuitry isgenerally any piece of computer hardware that is capable of processinginformation such as, for example, data, computer programs and/or othersuitable electronic information. The processing circuitry is composed ofa collection of electronic circuits some of which may be packaged as anintegrated circuit or multiple interconnected integrated circuits (anintegrated circuit at times more commonly referred to as a “chip”). Theprocessing circuitry may be configured to execute computer programs,which may be stored onboard the processing circuitry or otherwise storedin the memory 528 (of the same or another apparatus).

The processing circuitry 310 may be a number of processors, a multi-coreprocessor or some other type of processor, depending on the particularimplementation. The processing circuitry may include a graphicprocessing unit (GPU), a central processing unit (CPU), or a combinationof GPU and CPU. Further, the processing circuitry may be implementedusing a number of heterogeneous processor systems in which a mainprocessor is present with one or more secondary processors on a singlechip. As another illustrative example, the processing circuitry may be asymmetric multi-processor system containing multiple processors of thesame type. In yet another example, the processing circuitry may beembodied as or otherwise include one or more ASICs, FPGAs or the like.Thus, although the processing circuitry may be capable of executing acomputer program to perform one or more functions, the processingcircuitry of various examples may be capable of performing one or morefunctions without the aid of a computer program. In either instance, theprocessing circuitry may be appropriately programmed to performfunctions or operations according to example implementations of thepresent disclosure.

The memory 528 is generally any piece of computer hardware that iscapable of storing information such as, for example, data, computerprograms (e.g., computer-readable program code 530) and/or othersuitable information either on a temporary basis and/or a permanentbasis. The memory may include volatile and/or non-volatile memory, andmay be fixed or removable. Examples of suitable memory include randomaccess memory (RAM), read-only memory (ROM), a hard drive, a flashmemory, a thumb drive, a removable computer diskette, an optical disk, amagnetic tape or some combination of the above. Optical disks mayinclude compact disk-read only memory (CD-ROM), compact disk-read/write(CD-R/W), DVD or the like. In various instances, the memory may bereferred to as a computer-readable storage medium. The computer-readablestorage medium is a non-transitory device capable of storinginformation, and is distinguishable from computer-readable transmissionmedia such as electronic transitory signals capable of carryinginformation from one location to another. Computer-readable medium asdescribed herein may generally refer to a computer-readable storagemedium or computer-readable transmission medium.

In addition to the memory 528, as descried above, the processingcircuitry 310 may also be connected to one or more interfaces fordisplaying, transmitting and/or receiving information. The interfacesmay include the communications interface 312, and perhaps also thesecond communication interface 314. The communications interface(s) maybe configured to transmit and/or receive information, such as to and/orfrom other edge computing systems 208, remote stations 316 or the like.The communications interface(s) may be configured to transmit and/orreceive information by physical (wired) and/or wireless communicationslinks. These physical (wired) communication links in particular may beconfigured to implement any of a number of different technologies suchas RS-485, controller area network (CAN) bus or the like. Likewise,wireless communication links in particular may be configured toimplement any of a number of different radio access technologies such asany of a number of 3GPP or 4GPP radio access technologies, UMTS UTRA,GSM radio access technologies, CDMA 2000 radio access technologies,WLANs (e.g., IEEE 802.xx, e.g., 802.11a, 802.11b, 802.11g, 802.11n),WiMAX, IEEE 802.16, wireless PANs (WPANs) (e.g., IEEE 802.15,Bluetooth®, low power versions of Bluetooth®, IrDA, UWB, Wibree,Zigbee®), near-field communication technologies, and the like.

The processing circuitry 310 may also be connected to an IMU 324 and oneor more navigation sensors 326. The IMU may include one or more sensorssuch as accelerometers and gyroscopes, and may also includemagnetometers. As indicated above, the navigation sensor(s) may likewiseinclude a magnetometer. Other examples of suitable navigation sensorsinclude a barometer, satellite-based navigation receiver (e.g., GPS,GLONASS) and the like.

As indicated above, program code instructions may be stored in memory,and executed by processing circuitry that is thereby programmed, toimplement functions of the systems, subsystems, tools and theirrespective elements described herein. As will be appreciated, anysuitable program code instructions may be loaded onto a computer orother programmable apparatus from a computer-readable storage medium toproduce a particular machine, such that the particular machine becomes ameans for implementing the functions specified herein. These programcode instructions may also be stored in a computer-readable storagemedium that can direct a computer, a processing circuitry or otherprogrammable apparatus to function in a particular manner to therebygenerate a particular machine or particular article of manufacture. Theinstructions stored in the computer-readable storage medium may producean article of manufacture, where the article of manufacture becomes ameans for implementing functions described herein. The program codeinstructions may be retrieved from a computer-readable storage mediumand loaded into a computer, processing circuitry or other programmableapparatus to configure the computer, processing circuitry or otherprogrammable apparatus to execute operations to be performed on or bythe computer, processing circuitry or other programmable apparatus.

Retrieval, loading and execution of the program code instructions may beperformed sequentially such that one instruction is retrieved, loadedand executed at a time. In some example implementations, retrieval,loading and/or execution may be performed in parallel such that multipleinstructions are retrieved, loaded, and/or executed together. Executionof the program code instructions may produce a computer-implementedprocess such that the instructions executed by the computer, processingcircuitry or other programmable apparatus provide operations forimplementing functions described herein.

Execution of instructions by a processing circuitry, or storage ofinstructions in a computer-readable storage medium, supportscombinations of operations for performing the specified functions. Inthis manner, an edge computing system 208 may include processingcircuitry 310 and a computer-readable storage medium or memory 528coupled to the processing circuitry, where the processing circuitry isconfigured to execute computer-readable program code 530 stored in thememory. It will also be understood that one or more functions, andcombinations of functions, may be implemented by special purposehardware-based apparatuses and/or processing circuitry s which performthe specified functions, or combinations of special purpose hardware andprogram code instructions.

Many modifications and other implementations of the disclosure set forthherein will come to mind to one skilled in the art to which thedisclosure pertains having the benefit of the teachings presented in theforegoing description and the associated figures. Therefore, it is to beunderstood that the disclosure is not to be limited to the specificimplementations disclosed and that modifications and otherimplementations are intended to be included within the scope of theappended claims. Moreover, although the foregoing description and theassociated figures describe example implementations in the context ofcertain example combinations of elements and/or functions, it should beappreciated that different combinations of elements and/or functions maybe provided by alternative implementations without departing from thescope of the appended claims. In this regard, for example, differentcombinations of elements and/or functions than those explicitlydescribed above are also contemplated as may be set forth in some of theappended claims. Although specific terms are employed herein, they areused in a generic and descriptive sense only and not for purposes oflimitation.

What is claimed is:
 1. A multi-rotor vehicle comprising: an airframe;and coupled to the airframe, a plurality of electric motors operativelycoupled to a respective plurality of rotors, the plurality of electricmotors configured to cause the respective plurality of rotors to rotaterelative to the airframe; and a plurality of edge computing systems thatare independent, distinct and distributed to the plurality of electricmotors, each edge computing system of the plurality of edge computingsystems operatively coupled to a respective electric motor of theplurality of electric motors, and thereby a respective rotor of therespective plurality of rotors, each edge computing system configured toacquire and process sensor data for the respective rotor to determinerotor status information, and execute motor commands to control therespective electric motor and thereby the respective rotor, wherein eachedge computing system is configured as an integrated flight computer andmotor controller.
 2. The multi-rotor vehicle of claim 1, wherein eachedge computing system includes first power distribution circuitry forthe flight computer, and second power distribution circuitry for themotor controller.
 3. The multi-rotor vehicle of claim 2, wherein eachedge computing system further includes a power inverter circuit coupledto the second power distribution circuitry, the power inverter circuitconfigured to supply power to the respective electric motor of the edgecomputing system.
 4. The multi-rotor vehicle of claim 1, wherein eachedge computing system includes: processing circuitry configured toacquire and process the sensor data for the respective rotor todetermine rotor status information, and execute the motor commands tocontrol the respective electric motor and thereby the respective rotor;and a communication interface configured to enable the edge computingsystem to communicate with others of the plurality of edge computingsystems.
 5. The multi-rotor vehicle of claim 4, wherein the plurality ofedge computing systems are configured according to a model in which anyof the plurality of edge computing systems is selectable as a primaryedge computing system, and the plurality of edge computing systems otherthan the primary edge computing system are operable as secondary edgecomputing systems, the secondary edge computing systems configured tocommunicate respective rotor status information to the primary edgecomputing system, and the primary edge computing system configured toprovide the motor commands to the secondary edge computing systems. 6.The multi-rotor vehicle of claim 5, wherein each edge computing systemfurther includes a second communication interface configured to enablethe edge computing system to communicate with a remote station, theprimary edge computing system among the plurality of edge computingsystems being configured to communicate with the remote station.
 7. Themulti-rotor vehicle of claim 5, wherein the processing circuitry of eachedge computing system further includes a clock to measure and keep timeat the edge computing system, the secondary edge computing systemsconfigured to communicate with the primary edge computing system viarespective communication interfaces to synchronize respective clocks ofthe secondary edge computing systems with the clock of the primary edgecomputing system.
 8. The multi-rotor vehicle of claim 5, wherein theprimary edge computing system is configured to implement the flightcomputer to determine attitude, position and heading of the multi-rotorvehicle, and provide the motor commands based on the rotor statusinformation for the respective plurality of rotors, and the attitude,position and heading.
 9. The multi-rotor vehicle of claim 8, whereineach edge computing system includes an inertial measurement unit (IMU)and magnetometer, and the IMU and magnetometer of the primary edgecomputing system are configured to determine the attitude, position andheading of the multi-rotor vehicle.
 10. The multi-rotor vehicle of claim5, wherein each edge computing system is configured to store aconfiguration file with an ordered list of the plurality of edgecomputing systems that begins with the primary edge computing system andthen a first of the secondary edge computing systems, and wherein theprimary edge computing system is configured to communicate health statusinformation to the first of the secondary edge computing systems, and inresponse, the first of the secondary edge computing systems isconfigured to determine a health status of the primary edge computingsystem from the health status information, and assume responsibility asthe primary edge computing system when the health status reaches apredetermined threshold.
 11. The multi-rotor vehicle of claim 10,wherein the ordered list includes a second of the secondary edgecomputing systems after the first of the secondary edge computingsystems, and wherein after the first of the secondary edge computingsystems assumes responsibility as the primary edge computing system, thesecond of the secondary edge computing systems assumes responsibility asthe first of the secondary edge computing systems.
 12. An edge computingsystem of a plurality of edge computing systems configured for use on amulti-rotor vehicle including a plurality of electric motors operativelycoupled to a respective plurality of rotors, the plurality of electricmotors configured to cause the respective plurality of rotors to rotaterelative to an airframe, the plurality of edge computing systems beingindependent, distinct and distributable to the plurality of electricmotors, the edge computing system comprising: processing circuitryoperatively coupleable to a respective electric motor of the pluralityof electric motors, and thereby a respective rotor of the respectiveplurality of rotors, the processing circuitry configured to acquire andprocess sensor data for the respective rotor to determine rotor statusinformation, and execute motor commands to control the respectiveelectric motor and thereby the respective rotor; and a communicationinterface configured to enable the edge computing system to communicatewith others of the plurality of edge computing systems, wherein the edgecomputing system is configured as an integrated flight computer andmotor controller.
 13. The edge computing system of claim 12, wherein theedge computing system further comprises first power distributioncircuitry for the flight computer, and second power distributioncircuitry for the motor controller.
 14. The edge computing system ofclaim 13, wherein the edge computing system further comprises a powerinverter circuit coupled to the second power distribution circuitry, thepower inverter circuit configured to supply power to the respectiveelectric motor of the edge computing system.
 15. The edge computingsystem of claim 12, wherein the edge computing system is configured tocommunicate with the others of the plurality of edge computing systemsaccording to a model in which any of the plurality of edge computingsystems is selectable as a primary edge computing system, and theplurality of edge computing systems other than the primary edgecomputing system are operable as secondary edge computing systems, thesecondary edge computing systems configured to communicate respectiverotor status information to the primary edge computing system, and theprimary edge computing system configured to provide the motor commandsto the secondary edge computing systems.
 16. The edge computing systemof claim 15, wherein the edge computing system further comprises asecond communication interface configured to enable the edge computingsystem to communicate with a remote station, the primary edge computingsystem among the plurality of edge computing systems being configured tocommunicate with the remote station.
 17. The edge computing system ofclaim 15, wherein the processing circuitry of the edge computing systemfurther includes a clock to measure and keep time at the edge computingsystem, the secondary edge computing systems configured to communicatewith the primary edge computing system via respective communicationinterfaces to synchronize respective clocks of the secondary edgecomputing systems with the clock of the primary edge computing system.18. The edge computing system of claim 15, wherein the primary edgecomputing system is configured to implement the flight computer todetermine attitude, position and heading of the multi-rotor vehicle, andprovide the motor commands based on the rotor status information for therespective plurality of rotors, and the attitude, position and heading.19. The edge computing system of claim 18, wherein the edge computingsystem further comprises an inertial measurement unit (IMU) andmagnetometer, and the IMU and magnetometer of the primary edge computingsystem are configured to determine the attitude, position and heading ofthe multi-rotor vehicle.
 20. The edge computing system of claim 15,wherein the edge computing system is configured to store a configurationfile with an ordered list of the plurality of edge computing systemsthat begins with the primary edge computing system and then a first ofthe secondary edge computing systems, and wherein the primary edgecomputing system is configured to communicate health status informationto the first of the secondary edge computing systems, and in response,the first of the secondary edge computing systems is configured todetermine a health status of the primary edge computing system from thehealth status information, and assume responsibility as the primary edgecomputing system when the health status reaches a predeterminedthreshold.
 21. The edge computing system of claim 20, wherein theordered list includes a second of the secondary edge computing systemsafter the first of the secondary edge computing systems, and whereinafter the first of the secondary edge computing systems assumesresponsibility as the primary edge computing system, the second of thesecondary edge computing systems assumes responsibility as the first ofthe secondary edge computing systems.
 22. A method of operating amulti-rotor vehicle including a plurality of electric motors operativelycoupled to a respective plurality of rotors, and a plurality of edgecomputing systems that are independent, distinct and distributed to theplurality of electric motors, each edge computing system of theplurality of edge computing systems operatively coupled to a respectiveelectric motor of the plurality of electric motors, and thereby arespective rotor of the respective plurality of rotors, the methodcomprising each edge computing system: acquiring and processing sensordata for the respective rotor to determine rotor status information; andexecuting motor commands to control the respective electric motor andthereby the respective rotor, wherein each edge computing system isconfigured as an integrated flight computer and motor controller. 23.The method of claim 22, wherein each edge computing system includesfirst power distribution circuitry for the flight computer, second powerdistribution circuitry for the motor controller, and a power invertercircuit coupled to the second power distribution circuitry, and themethod further comprises the power inverter circuit supplying power tothe respective electric motor of the edge computing system.
 24. Themethod of claim 22, wherein the plurality of edge computing systems areconfigured according to a model in which any of the plurality of edgecomputing systems is selectable as a primary edge computing system, andthe plurality of edge computing systems other than the primary edgecomputing system are operable as secondary edge computing systems, themethod further comprising the secondary edge computing systemscommunicating respective rotor status information to the primary edgecomputing system, and the primary edge computing system providing themotor commands to the secondary edge computing systems.
 25. The methodof claim 24, wherein each edge computing system is enabled tocommunicate with a remote station, and the method further comprises theprimary edge computing system among the plurality of edge computingsystems communicating with the remote station.
 26. The method of claim24, wherein each edge computing system includes a clock to measure andkeep time at the edge computing system, and the method further comprisesthe secondary edge computing systems communicating with the primary edgecomputing system to synchronize respective clocks of the secondary edgecomputing systems with the clock of the primary edge computing system.27. The method of claim 24, wherein the method further comprises theprimary edge computing system implementing the flight computer todetermine attitude, position and heading of the multi-rotor vehicle, andproviding the motor commands based on the rotor status information forthe respective plurality of rotors, and the attitude, position andheading.
 28. The method of claim 27, wherein each edge computing systemincludes an inertial measurement unit (IMU) and magnetometer, and themethod further comprises the IMU and magnetometer of the primary edgecomputing system determining the attitude, position and heading of themulti-rotor vehicle.
 29. The method of claim 24, wherein each edgecomputing system is configured to store a configuration file with anordered list of the plurality of edge computing systems that begins withthe primary edge computing system and then a first of the secondary edgecomputing systems, and wherein the method further comprises the primaryedge computing system communicating health status information to thefirst of the secondary edge computing systems, and in response, thefirst of the secondary edge computing systems determining a healthstatus of the primary edge computing system from the health statusinformation, and assuming responsibility as the primary edge computingsystem when the health status reaches a predetermined threshold.
 30. Themethod of claim 29, wherein the ordered list includes a second of thesecondary edge computing systems after the first of the secondary edgecomputing systems, and wherein the method further comprises, after thefirst of the secondary edge computing systems assumes responsibility asthe primary edge computing system, the second of the secondary edgecomputing systems assuming responsibility as the first of the secondaryedge computing systems.